Improving the Prediction for the NASA High-Lift Trap Wing Model-Reference-Cited by-同舟云学术

Improving the Prediction for the NASA High-Lift Trap Wing Model

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Eliasson Peter¹,Peng Shia-Hui¹,Hanifi Ardeshir²

Affiliation:

1. Swedish Defense Research Agency (FOI)

2. FOI, Swedish Defence Research Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-867

Reference30 articles.

1. Evaluation of CFD methods for transport aircraft high lift systems

2. 2Rudnik, R., von Geyr, H. "The European High Lift Project EUROLIFT II -Objectives, Approach, and Structure", AIAA Paper 2007-4296.

3. 3Quix, H.,Schulz,M., Quest, J."LowSpeed High Lift ValidationTests withinthe European Project EUROLIFT II", AIAA Paper 2007-4296.

4. 4von Geyr, H., Schade, N., van der Burg, J.W., Eliasson, P., Esquieu, S. "CFD Prediction of Maximum Lift Effects on Realistic High-Lift-Commercial-Aircraft-Configurations withinthe Europeanproject EUROLIFTII", AIAAPaper 2007-4299.

5. 5Wild, J., Brezillon, J., Amoignon, O., Quest, J., Moens, F., Quagliarella, D. "Advanced High-Lift Design by Numerical Methods and Wind Tunnel Verification withintheEuropean ProjectEUROLIFT II", AIAA Paper 2007-4300.

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Results from the Second AIAA CFD High-Lift Prediction Workshop Using Edge;Journal of Aircraft;2015-07

2. Japan Aerospace Exploration Agency Studies for the Second High-Lift Prediction Workshop;Journal of Aircraft;2015-07

3. Overview and Summary of the Second AIAA High-Lift Prediction Workshop;Journal of Aircraft;2015-07

4. NASA Trapezoidal Wing Computations Including Transition and Advanced Turbulence Modeling;Journal of Aircraft;2015-03

5. Numerical Investigation of Wall Mounting Effects in Semi-Span Wind-Tunnel Tests;53rd AIAA Aerospace Sciences Meeting;2015-01-02